METHOD AND APPARATUS FOR CONTROL OF A STEERABLE LANDING GEAR

A slip-reduction control unit for an aircraft having a steerable landing gear. The control unit receives steering input signals from which a target steering command output may be ascertained and additional input signals (a) the motion of the aircraft, (b) a steering angle, or (c) a parameter relatin...

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Bibliographische Detailangaben

Hauptverfasser:	ROMANA Louis-Emmanuel, MAYOLLE Matthieu, GARAYGAY Cecile
Format:	Patent
Sprache:	eng
Schlagworte:	AEROPLANES AIRCRAFT AVIATION CONTROLLING COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS PHYSICS REGULATING SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES TRANSPORTING
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